TCDS G1IN

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION G1IN Revision 4 SCHEMPP-HIRTH Standard Austria S Standard Austria SH Standard Austria SH1 February 10, 2022 TYPE CERTIFICATE DATA SHEET NO. G1IN This Data Sheet which is a part of Type Certificate No. G1IN prescribes conditions and limitations under which the product for which the type certificate was issued meets the Airworthiness Requirements of the Federal Aviation Administration. Type Certificate Holder: Schempp-Hirth Flugzeugbau GmbH Krebenstrasse 25 73230 Kirchheim/Teck Germany Type Certificate Holder Record: SHK Segelflugzeugbau GmbH transferred TC G1IN to Schempp-Hirth Flugzeugbau GmbH on January 16, 1981. Schempp-Hirth K.G. transferred TC G1IN to SHK Segelflugzeugbau GmbH on April 6, 1976. I - Model Standard Austria S Glider, Approved October 27, 1962; Models Standard Austria SH and Standard Austria SH1 Gliders, Approved July 20, 1964 Airspeed Limits: Glide or dive 135 knots Max. speed in rough air 75 knots Airplane tow 75 knots Auto-winch tow 54 knots Airbrakes extended 118 knots C.G. Range: Models S and SH (+14.2) to (+18.1) Model SH1 (+14.2) to (+19.7) Datum: Wing leading edge at rib 1 Leveling Means: Model S: Top edge of fuselage horizontal Model SH & SH1: Fuselage-centerline horizontal (slope of top edge fuselage/ 100 to 8) Maximum Weight: 772 lbs No. of Seats: 1 Baggage: None Control Surface Movements: Elevator Up Down 120 mm +0/ -5 (4.73 in +0/ -.20) 75 mm ±5 (2.95 in ±.20) Page No. 1 2 Rev. No. 4 4 G1IN 2 Rudder Up 90 mm ±5 (3.54 in ±.20) Down 90 mm ±5 (3.54 in ±.20) Aileron Up 120 mm +0/ -5 (4.73 in +0/ -.20) Down 50 mm +0/ -2 (1.97 in +0/ -.08) For elevator, rudder and aileron measuring point, see Flight Manual Serial Nos. Eligible: The NAA Export Certificate of Airworthiness (Export C of A) endorsed as noted below under "Import Requirements" must be submitted for each individual glider for which application for certification is made. Import Requirements: A U.S. Airworthiness Certificate may be issued on the basis of an NAA Export C of A signed by a representative of the German Airworthiness Authority, the Luftfahrt-Bundesamt (LBA), containing the following statement: "The glider covered by this certificate has been examined and found to comply fully with the Federal Republic of Germany Glider Airworthiness Requirements dated August 1939, and conforms to Type Certificate No. G1IN." (This certification is equivalent to CAR 5 effective February 15, 1956.) Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. Certification Basis: CAR 10. Type Certificate No. G1IN issued October 27, 1962. Application for Type Certificate dated March 4, 1962. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the glider for certification. Model SH same as model S except for wing-profile Eppler 266, instead of NACA 652-415 and minor modifications. Model SH1 same as model SH except for retractable landing wheel. NOTES. NOTE 1. Current weight and balance report including list of equipment in certificated empty weight, and loading instructions when necessary, must be provided for each glider at the time of original certification. NOTE 2. The following placards must be installed in full view of the pilot: (a) "Cloud flying”: Permitted only when the following instruments are installed: (1) Altimeter (approved type) (2) Turn and bank (approved type) (3) Variometer (4) Compass" (b) "When flying in rough air do not exceed 75 knots (87 m.p.h.)" (c) "Night flying is prohibited." ...END...